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208                  Chapter 11  Incompressible Flow Analysis



                              11.1  Basic Equations

                                  11.1.1  Differential Equations
                                         The flow behavior in three dimensions is governed by
                              the full Navier-Stokes equations consisting of the conservation of
                              mass,  momentums  and  energy.    There  are  five  differential  equa-
                              tions  which  are  coupled  in  complicated  form.    Solving  the  full
                              Navier-Stokes  equations  requires  extensive  computational  effort.
                              The  equations  are  thus  normally  reduced  into  simplified  forms
                              according to different classes of flow behaviors.
                                         In this chapter, we will concentrate on the steady-state
                              incompressible laminar flow analysis in two-dimensional Cartesian
                              coordinates.  The Navier-Stokes equations, in this case, consist of
                              only three differential equations.  These equations are: (a) conser-
                              vation of mass, (b) conservation of momentum in the x-direction,
                              and (c) conservation of momentum in the y-direction as follows.
                                                      u       v         0
                                                      x     y 
                                                           p          u         u 
                                           
                                                                             
                                                                
                                   (    ) uu     (    ) vu                       
                                  x          y             x    x     x     y       y     
                                                           p          v         v 
                                           
                                   (    ) uv      (    ) vv                         
                                  x          y             y    x     x     y       y     
                              where    is  the  density,  u  and  v  are  the  velocity  components  in
                              the  x-  and  y-directions,  respectively,  p  is  the  pressure,  and    is
                              the dynamic viscosity.
                                         The  three  basic  unknowns  of  the  three  differential
                              equations  above  are  the  velocity  components  (, ),ux y   (, )vx y  and
                              pressure  (, )p xy .  It is noted that the differential equations form a
                              set  of  coupled  nonlinear  differential  equations.    Such  the  set  of
                              differential equations is more difficult to solve as compared to the
                              differential equations in the preceding chapters.
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